N602AW

Part: HANDLE — OUT OF ADJUST (L2 DOOR) · airframe 58,351 hrs · 23,016 cycles

FLIGHT ATTENDANT UNABLE TO ARM DOOR 2L. ADJUSTED ESCAPE SLIDE HANDLE IAW AMM 52-11-22-820-11 & LUBED CABLE. REMOVED & INSTALLED SLIDE IAW AMM 25-62-44.

Part: RIB — CRACKED (NR 1 PYLON) · airframe 58,263 hrs · 22,978 cycles

NUMBER 1 ENG PYLON RIB 4 IS CRACKED ON INNER & OUTER SIDE OF RADIUS AT LOWER END. REMOVED, WELDED & REINSTALLED PYLON RIB NR 4 IAW SRM 51-42-11 & 54-30-00-101.

Part: SIGN — NOT SEATED (CABIN) · airframe 58,239 hrs · 22,967 cycles

EXIT SIGN IS BURNT OUT. RESEATED EXIT SIGN 1L DOOR OPERATIONS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 57,460 hrs · 22,678 cycles

EMERGENCY LIGHT LENS COVER MISSING FROM SEAT ROW 7 LT. INSTALLED EMER LIGHT LENS AT SEAT ROW 7 LT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 57,261 hrs · 22,592 cycles

EN ROUTE CREW RECEIVED STATUS MSG INOP SYS. REVERSER 1 ENG 1 THRUST, FLIGHT DIVERTED. FOUND NO FAULTS ON PFR OR MSG. PERFORMED OPERATIONAL TEST OF NR 1 ENG THRUST REVERSER IAW AMM 78-31-00-710-041-A 13, TESTED OK. PERFORMED TSM 76-00-00-810-803-A WITH NR 1 ENG RUN. NO FAULTS, OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 57,190 hrs · 22,566 cycles

IN CRUISE FLIGHT AT FL 350 STATUS MSG APPEARED. WHEN SLATS OUT ENG 1 AT IDLE ON GND ENG 1 MAX PWR, IDLE " $ INOP SYS REVERSER NR 1 ENG 1 THRUST. PERFORMED BITE TEST OF NR 1 ENG FADEC IAW AMM 73-22-00-710-040-A, TEST PASSED. PERFORMED BITE TEST OF ENG 1 INTERFACE UNIT IAW AMM 73-25-34-710-042-A, TEST PASSED. PERFORMED BITE TEST OF CENTRAL WARNING SYS IAW AMM 31-50-00-710-001-A, TEST PASSED. NO HISTORY ON THRUST REVERSERS PAST 30 DAYS. NO CLASS 1 WARNING IN PFR. ACFT OK FOR RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,036 hrs · 22,494 cycles

AFT EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN AFT EMER FLASHLIGHT.

Part: LENS — MISSING (CABIN) · airframe 55,788 hrs · 22,023 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHT MISSING LENS AT ROW 9 LT. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT LENS AT ROW 9 LT.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 55,535 hrs · 21,941 cycles

AFT MEGA PHONE DAMAGED. REPLACED AFT MEGA PHONE, OPERATIONS CHECKED GOOD.

Part: LENS — LOOSE (EXIT SIGN) · airframe 55,298 hrs · 21,858 cycles

EXIT SIGN LENS AT DOOR 2R BY FLOOR HAS COVER LOOSE. REPLACED EXIT SIGN LENS AT DOOR 2R.

Part: PRESSURE SWITCH — INOPERATIVE (HYDRAULIC SYS) · airframe 54,865 hrs · 21,707 cycles

SHORTLY AFTER TAKEOFF GOT GREEN HYD ENG 1 PUMP FAULT. REPLACED NR 1 ENG HYD PUMP PRESS SWITCH IAW A320 AMM 29-11-17.

Part: LIGHT — UNSECURE (CABIN) · airframe 54,622 hrs · 21,615 cycles

CREW REPORTED THE EMERGENCY LIGHT IN REAR GALLEY BROKEN. MAINTENANCE SECURED REAR GALLEY EMERGENCY LIGHT.

Part: BRACKET — UNSECURE (ZONE 200) · airframe 54,612 hrs · 21,610 cycles

CREW REPORTED SEAT 9D FLOOR LIGHT DANGLING. MX SECURED SEAT MOUNTED EXIT LIGHT BRACKET ON SEAT 9D. OPS CHECKED GOOD IAW CMM 25-27-35.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,205 hrs · 21,464 cycles

LEFT FORWARD EMERGENCY LIGHT FAILED TEST. R & R LT FORWARD EMERGENCY BATTERY.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 53,953 hrs · 21,384 cycles

R2 DOOR EXIT LIGHT LENS BROKEN. INSTALLED NEW EXIT LIGHT LENS AT R2 DOOR.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,684 hrs · 21,308 cycles

L2 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED L2 DOOR EMERGENCY LIGHT LENS.

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHTS) · airframe 53,569 hrs · 21,277 cycles

MX REPORTED THE EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. MX REPLACED EMERGENCY LIGHT HARNESS AT SEAT 26L. OPS CHECKED GOOD. IAW ESPM 20-33-22.

Part: LENS — BROKEN (CABIN) · airframe 53,099 hrs · 21,126 cycles

EXIT ROW LIGHT BROKE OFF AT 1C. REPLACED LENS AT 1C EMERGENCY LIGHT.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 52,703 hrs · 20,995 cycles

SEAT ROW 22L EMERGENCY CONNECTOR PLUG PULLED OUT FROM SPLICES. REMOVED AND REPLACED SEAT HARNESS.

Part: LENS — MISSING (CABIN) · airframe 52,269 hrs · 20,868 cycles

RIGHT REAR EXIT DOOR EMERGENCY LIGHT CASING MISSING. REPLACED MISSING LENS AT RIGHT REAR DOOR.

Part: LENS — MISSING (CABIN) · airframe 51,771 hrs · 20,699 cycles

EXIT LIGHT COVER 2L DOOR MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS COVER AT DOOR 2L.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,811 hrs · 20,370 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY NEEDS REPLACING. REPLACED AFT F/A FLASHLIGHT BATTERY - OPERATIONAL CHECK NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 50,456 hrs · 20,251 cycles

EMERGENCY EXIT LIGHT AT ROW 10 RIGHT IS INOPERATIVE. FOUND WIRE DISCONNECTED FROM LIGHT. RECONNECTED TERMINAL FITTING TO LIGHT. OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 49,873 hrs · 20,061 cycles

OVERWING EMERGENCY EXIT LIGHT MISSING ROW 10 AIRCRAFT RIGHT LOWER SIDE PANEL. RE-INSTALLED EMERGENCY LIGHT ASSEMBLY AND APPLIED TAPE TO DAMAGED AREA OF PANEL. EMERGENCY LIGHTS OPS CHECK NORMAL.

Part: ATTACH FITTING — CORRODED (RT WING) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON FORWARD LUG OF RIGHT WING BOX MAIN LANDING GEAR ATTACHMENT FITTING RIB 5 GEAR SUPPORT WS 2508. REPAIRED FORWARD LUG OF RIGHT WING BOX MAIN LANDING GEAR ATTACHMENT FITTING IAW EA 501967.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - OUT OF ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER AND FINGER AT PASSENGER DOOR 842 (R2). PERFORMED ADJUSTMENT OF DIMENSION "A" BETWEEN STRIKER LEVER AND FINGER AT PASSENGER DOOR 842 (R2) IAW A320 AMM 52-13-14-820-002-A ITEM 4A STEP 2.

Part: SLIDE — BULGED (CABIN) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - DURING A DVI OF THE LEFT OFF WING SLIDE ENCLOSURE DOOR FOUND IT NOT FLUSH WITH THE OUTER SURFACE OF THE LEFT OFF WING SLIDE ENCLOSURE. REPACKED LEFT OFF WING SLIDE IAW CMM 25-60-58 REV 18 AND FOLDING PROCEDURES P-11907 REV R.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON FORWARD CURVE EDGE OF THE LEFT AFT EMERGENCY EXIT DOOR (834) AT FR40. REPLACED FORWARD CURVE EDGE OF THE LEFT AFT EMERGENCY EXIT DOOR (834) AT FR40 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D52279010.

Part: DOOR FRAME — CORRODED (ESCAPE HATCH) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4. REPLACED CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4 IAW A320 SRM 51-72-11 DRAWING D52279010.

Part: FITTING — CORRODED (RT PLYON) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON RIGHT PYLON SPIGOT FITTING BETWEEN PYLON STA 4697 TO STA 4954, & BETWEEN RIB 5 TO RIB 4. REPLACED RIGHT PYLON SPIGOT FITTING IAW A320 SRM 54-51-12.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - DELAMINATION ON FLOOR PANEL 232PF BETWEEN FR24 TO FR28, BETWEEN Y-1732 TO Y-1292. REPLACED FLOOR PANEL 232PF IAW A320 SRM 53-02-00, TABLE 103 AND IRM 9701 REV G.

Part: COUPLING — ELONGATED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR 23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D53474250.

Part: COUPLING — ELONGATED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR 23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D53474250.

Part: COUPLING — ELONGATED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D53474250.

Part: COUPLING — ELONGATED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D53474250.

Part: WEB — CRACKED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CRACK IN WEB BETWEEN FR8 TO FR11, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110285.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON SHEAR PLATE ASSEMBLY BETWEEN FR58 TO FR59, S38R. REPLACED SHEAR PLATE ASSEMBLY BETWEEN FR58 TO FR59, S38R IAW A320 SRM 51-72-11AND DRAWING D53475750.

Part: COUPLING — CORRODED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON INBOARD UPPER COUPLING AT FR66, S23L, Y1450. REPLACED INBOARD UPPER COUPLING AT FR66, S23L, Y1450 IAW A320 A320 51-42-11 AND DRAWING D53474250.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR25, S41L. REPLACED SHEAR TIE AT FR25, S41L IAW A320 SRM 51-72-11.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF RIGHT AFT EMERGENCY EXIT HATCH (844) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF LEFT FORWARD EMERGENCY EXIT HATCH (833) BETWEEN FR38 TO FR39 & BETWEEN BEAM 4 AND EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CRACK ON INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF LEFT AFT EMERGENCY EXIT HATCH (834) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.

Part: COUPLING — CORRODED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON INBOARD LOWER COUPLING AT FR66, S23L, Y1450. REPLACED INBOARD LOWER COUPLING AT FR66, S23L, Y1450 IAW A320 SRM 51-42-11 AND DRAWING D53474250.

Part: DOOR FRAME — CORRODED (ESCAPE HATCH) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4. REPLACED CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4 IAW A320 SRM 51-72-11 DRAWING D52279010.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR65 TO FR66, S23L. REPLACED WEB BETWEEN FR65 TO FR66, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D534474250.

Part: SPAR — CORRODED (TE FLAP) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FRONT SPAR OF OUTBOUND FLAP LEADING EDGE BETWEEN WS 7792 TO WS 8268, RIB 14 TO RIB 15. REPLACED LEFT WING FRONT SPAR OF OUTBOUND FLAP LEADING EDGE BETWEEN WS 7792 TO WS 8268, RIB 14 TO RIB 15 IAW A320 SRM 51-72-11 AND DRAWING D57571206.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON T-SECTION ANGLE OF AFT LOWER VERTICAL FRAME OF LEFT FORWARD EMERGENCY EXIT HATCH (833) BETWEEN FR38 TO FR39 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CRACK IN INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 843 IAW EO 5210Y228.

Part: COUPLING — CORRODED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON OUTBOARD UPPER COUPLING AT FR66, S23L, Y1450. REPLACED OUTBOARD UPPER COUPLING AT FR66, S23L, Y1450 IAW A320 SRM 51-42-11 AND DRAWING D53474250.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR34, S43R. REPLACED SHEAR TIE AT FR34, S43R IAW A320 SRM 51-72-11.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CRACK ON INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CRACK ON SECTION CONNECTING AT FR68, S24L. REPLACED SECTION CONNECTING AT FR68, S24L IAW A320 SRM 51-72-11 AND DRAWING D53474250.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CRACK IN INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR65 TO FR66, S23R. REPLACED WEB BETWEEN FR65 TO FR66, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505 & D53474250.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - CORROSION ON T-SECTION ANGLE OF AFT LOWER VERTICAL FRAME OF RIGHT AFT EMERGENCY EXIT HATCH (844) BETWEEN FR40 TO FR41 & BETWEEN BEAM 4 & EDGE CURVE AREA. REPLACED T-SECTION ANGLE IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279040.

Part: COUPLING — CORRODED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON OUTBOARD LOWER COUPLING AT FR66, S23L, Y1450. REPLACED OUTBOARD LOWER COUPLING AT FR66, S23L, Y1450 IAW A320 SRM 51-42-11 AND DRAWING D53474250.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON LOWER DOOR SILL OF BULK CARGO COMPARTMENT AT FR 61+19 INCHES, S38R. REPLACED LOWER DOOR SILL OF BULK CARGO COMPARTMENT IAW A320 SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CORROSION ON SEAT TRACK BETWEEN FR56+9 INCHES TO FR59+3 INCHES, Y765. REPAIRED SEAT TRACK BETWEEN FR56+8 INCHES TO FR64, Y765 IAW A320 SRM 53-41-15 FIGURE 102 PAGES 215/216.

Part: SILL — CRACKED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - CRACK ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L IAW A320 SRM 51-72-11AND DRAWING D53480505.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SILL BETWEEN FR66 TO FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWINGS D53480505 & D53480076.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL FITTING BETWEEN FR16 TO FR20, S23R. REPLACED LOWER SILL FITTING BETWEEN FR16 TO FR20, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112320, D53112805 & EA 501956.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,772 hrs · 20,024 cycles

3S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR 66+6", -Y1732. REPLACED LOWER SILL BETWEEN FR66 TO FR 66+6", -Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWINGS D53480505 & EA 500738.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 4,977 hrs · 20,024 cycles

2S CHECK - EXCESSIVE PLAY AT RUDDER HINGE FITTING NR 2 AT VERTICAL STABILIZER STA 1926 RIB 4. REPLACED RUDDER HINGE FITTING NR 2 IAW A320 SRM 51-72-11 & AMM 55-36-41-400-001-A.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - DISBONDED FLOOR PANEL 151LF BETWEEN FR56 TO FR58, Y765 TO -Y765. REPLACED FLOOR PANEL 151LF IAW A320 SRM 53-02-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,772 hrs · 20,024 cycles

3S CHECK - DELAMINATION ON FLOOR PANEL 152MF BETWEEN FR56 TO FR58 & BETWEEN -Y765 TO -Y970.8. REPLACED FLOOR PANEL 152MF IAW A320 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - DELAMINATION ON FLOOR PANEL 131AF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 131AF IAW A320 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 4,977 hrs · 20,024 cycles

3S CHECK - DISBONDED FLOOR PANEL 151GF BETWEEN FR53 TO FR55, Y765 TO -Y765. REPLACED FLOOR PANEL 151GF IAW A320 SRM 53-02-00 AND IRM 9701 REV G.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,714 hrs · 20,003 cycles

EMERGENCY EXIT FLOOR PATH LIGHT SEAT 1C INOPERATIVE. REPAIRED EMERGENCY LIGHT ASSEMBLY AT SEAT 1C. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 49,539 hrs · 19,955 cycles

R2 DOOR ASSIST PRESSURE LOW. SERVICED R2 DOOR TO PROPER PRESSURE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: WIRE — BROKEN (CABIN) · airframe 49,081 hrs · 19,806 cycles

ROW 22 ABC EMERGENCY EXIT LIGHT INOP. RETERMINATED BROKEN WIRE TERMINAL AT SEAT LIGHT IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-25-22.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 49,026 hrs · 19,780 cycles

LAV E SMOKE DETECTION AURAL AND LIGHT ACTIVATED IN FLIGHT. NO SMOKE WAS FOUND. RESET AFT PANEL - AURAL AND LIGHT INDICATIONS EXTINGUISHED. CIDS PANEL LAV SMOKE ILLUMINATED. MAINTENANCE PERFORMED OPERATIONAL TEST OF THE LAV SMOKE DETECTION SYSTEM IAW AIRBUS MAINTENANCE MANUAL 26-17-00-710-001 WITH NO FAULTS NOTED.

Part: MEGAPHONE — NO TEST (CABIN) · airframe 48,767 hrs · 19,695 cycles

FLIGHT ATTENDANT REPORTED AFT MEGAPHONE FAILED PREFLIGHT TEST. MAINTENANCE REPLACED FORWARD MEGAPHONE.

Part: MEGAPHONE — BROKEN (CABIN) · airframe 48,550 hrs · 19,624 cycles

FORWARD MEGAPHONE HANDLE BROKEN. REPLACED FORWARD MEGAPHONE AS REQUIRED.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 48,550 hrs · 19,624 cycles

R2 DOOR BOTTLE ASSIST PRESSURE LOW. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 48,357 hrs · 19,563 cycles

ON TAKEOFF ROLL AT 65 KNOTS, ECAM CHIME WITH ENGINE 2 COMPRESSOR FAULT ON UPPER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING PER TROUBLESHOOTING MANUAL 75-30-00-810-84601 AND POWER ASSURANCE TEST PER AIRBUS MAINTENANCE MANUAL 71-00-00-710-013. NO FAULTS FOUND AND NO SUBSEQUENT ISSUES.

Part: LENS — MISSING (CABIN) · airframe 48,133 hrs · 19,488 cycles

DOOR 2L EMERGENCY EXIT LIGHT PLASTIC COVER MISSING. REPLACED EMERGENCY EXIT LIGHT PLASTIC LENS COVER AT 2L DOOR.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 47,331 hrs · 19,196 cycles

FLIGHT ATTENDANT REPORTED A BURNING PLASTIC ODOR EMANATING FROM FORWARD GALLEY. TURNED BOTH OVEN SWITCHES AND BUN WARMERS TO OFF - ODOR STILL PRESENT AT TIMES. NO SMOKE OR OTHER INDICATIONS ASSOCIATED WITH SMELL. MAINTENANCE REMOVED AND REPLACED NR 1 OVEN IN FORWARD GALLEY IAW AIRBUS MAINTENANCE MANUAL 25-35-19.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 46,606 hrs · 18,945 cycles

R-2 DOOR ASSIST BOTTLE PSI LOW. SERVICED R-2 DOOR ASSIST BOTTLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,825 hrs · 18,676 cycles

FLT 231 - PHX - EEL - AIRCRAFT LEFT OVERWING RED EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED LENS AND RELAMPED.

Part: FAN — FAULTY (CABIN) · airframe 45,481 hrs · 18,546 cycles

FLT 658 SFO-PHL - BURNING SMELL - AT CRUISE (340), CREW REPORTED STRONG SMELL OF INSULATION OR BURNING PLASTIC COMING FROM GASPER VENTS IN FLIGHT DECK. FLIGHT ATTENDANT REPORTED SMELL STRONGEST OVERWING. WHEN PACK 1 WAS TURNED OFF, SMELL INCREASED; PACK 2 OFF, ODOR CLEARED. MAINTENANCE TROUBLESHOT TO RIGHT RECIRCULATION FAN - REMOVED AND REPLACED FAN.

Part: WIRE — DAMAGED (CABIN) · airframe 45,179 hrs · 18,436 cycles

FLT 191 - PHX - EEL - EMERGENCY EXIT AISLE LIGHTS SEAT ROW 22 INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 22 LEFT EMERGENCY LIGHT.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 45,082 hrs · 18,402 cycles

FLT 187 - PHX - EEL - CIDS PANEL EMERGENCY LIGHT DOES NOT TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT LEFT CENTER CABIN POSITION IAW AIRBUS MAINTENANCE MANUAL 33-51-39.

Part: HINGE FITTING — WORN (FUSELAGE) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - DEEP WEAR ON LEFT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, Y230. REPAIRED LEFT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, Y230 IAW EA 116645.

Part: HINGE FITTING — WORN (FUSELAGE) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - DEEP WEAR ON RIGHT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, -Y230. REPAIRED RIGHT MAIN LANDING GEAR FORWARD HINGE ATTACH FITTING LUG AT FR42, -Y230 IAW EA 116646.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 251RF AT FORWARD OUTBOARD CORNER. REPLACED FLOOR PANEL 251RF IAW IAW MCGILL IRM 9701 REV G.

Part: FLAP — DELAMINATED (LT WING) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - DISBOND ON LEFT OUTBOARD FLAP TRAILING EDGE. REPAIRED LEFT OUTBOARD FLAP TRAILING EDGE IAW A320 SRM 57-53-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 221DF AT FR13, Y=0. REPLACED FLOOR PANEL 221DF IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 222EF. REPLACED FLOOR PANEL 222EF IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - UPPER SURFACE OF FLOOR PANEL 261QF PEELING AT FR13, Y=0 1 INCH FROM INBOARD EDGE & 1 INCH FROM AFT EDGE. REPLACED FLOOR PANEL 261QF IAW MCGILL IRM 9701 REV G.

Part: AILERON — CORRODED (LT WING) · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - CORROSION ON UPPER TRAILING EDGE OF LEFT AILERON. REPAIRED UPPER TRAILING EDGE OF LEFT AILERON IAW A320 SRM 57-61-21 REPAIR A FIGURE 212.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,445 hrs · 18,157 cycles

PIT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CHANNEL AT FR12, S12R. REPLACED CHANNEL AT FR12, S12R IAW A320 SRM 51-42-00 & 51-76-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,445 hrs · 18,157 cycles

PIT - MAJOR REPAIR - C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR 20, -Y254. REPAIRED FLOORBEAM AT FR 20, -Y254 IAW A320 SRM 53-53-00-14 FIG 204.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 44,122 hrs · 18,036 cycles

FLT 307 - LAS - EES - R2 DOOR ASSIST PRESSURE LOW. MAINTENANCE SERVICED R2 DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614.

Part: LIGHT — MISSING (CABIN) · airframe 43,750 hrs · 17,915 cycles

FLT 32 - PHX - EEL - ROW 10, A/C RIGHT, EMERGENCY EXIT LIGHT IS MISSING. MAINTENANCE FOUND EMERGENCY LIGHT HAD BEEN KNOCKED OUT OF SIDEWALL MOUNT. RE-INSTALLED LIGHT.

Part: OVEN — DIRTY (GALLEY) · airframe 43,368 hrs · 17,781 cycles

FLT 310 - LAX-CLT - BURNING SMELL - NR 2 OVEN FORWARD GALLEY MADE A LOUD NOISE & VIBRATION WHEN TURNED ON ACCOMPANIED BY STRONG CHEMICAL/PLASTIC SMELL. FLIGHT ATTENDANT TURNED OFF OVEN, NOISE AND VIBRATION AND SMELL STOPPED. REMOVED FOD FROM OVEN. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 41,906 hrs · 17,299 cycles

FLT 77 - SEA - EES - DOOR R-2 ASSIST BOTTLE PRESSURE IS LOW. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 41,906 hrs · 17,299 cycles

FLT 77 - SEA - EEL - AFT FLIGHT ATTENDANT LT STATION EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY.

Part: FLAP — OUT OF RIG (WING) · airframe 41,789 hrs · 17,255 cycles

FLT 614 - SLC-PHX - EMERGENCY LANDING - FLAPS LOCKED ON APPROACH. PERFORMED VISUAL INSPECTION OF ENTIRE LENGTH OF TORQUE SHAFT OF LEFT FLAP DRIVE SYSTEM. NO DEFECTS NOTED. WILL KEEP THIS SDR FILE OPEN TO CONTINUE MONITORING FOR POSSIBLE EVENTS FOR 10 DAYS. 2 MORE EVENTS OCCURRED FOR THE SAME ISSUE (FLAPS STOPPED AT POSITION 1). RIGGED THE LEFT FLAP PER AMM 27-51-44-820-001. OPERATIONAL CHECK PER AMM 27-51-00-820-003. OPERATIONAL CHECK WAS GOOD.

Part: DAMPENER — LOW PRESSURE (R2 DOOR) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 CHECK - EES - R2 DOOR ASSIST DAMPNER HAS LOW PRESSURE AND REQUIRES SERVICING. SERVICED THE R2 DOOR ASSIST DAMPNER IAW US AIRWAYS TASK CARD I1C52308.

Part: DAMPENER — LOW PRESSURE (L1 DOOR) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 CHECK - EES - L1 DOOR ASSIST DAMPNER HAS LOW PRESSURE AND REQUIRES SERVICING. SERVICED THE L1 DOOR ASSIST DAMPNER IAW A320 AMM 52-10-00.

Part: ANCHOR FITTING — CORRODED (RT MLG) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON LOWER FACE OF ANCHORAGE FITTING BS 1406 ON RIGHT MAIN LANDING GEAR. REPAIRED ANCHORAGE FITTING BS 1406 ON RIGHT MAIN LANDING GEAR IAW US AIRWAYS EA 132319.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON LOWER SILL OF R-2 DOOR AT FR67 +18 INCHES, S23R. REPAIRED LOWER SILL OF R-2 DOOR AT FR67 +18 INCHES, S23R IAW A320 SRM 53-41-14 REPAIR PRINCIPLE 5 & US AIRWAYS EA 132317.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR51 TO FR52, S38R. REPLACED SHEAR PLATE WEB BETWEEN FR51 TO FR52, S38R IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR50 TO FR51, S38R. REPLACED SHEAR PLATE WEB BETWEEN FR50 TO FR51, S38R IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR48 TO FR49, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR48 TO FR49, S38L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y1292 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON R-2 LOWER DOOR SILL BETWEEN FR66 TO FR67, -Y1732. REPAIRED R-2 LOWER DOOR SILL BETWEEN FR66 TO FR67, -Y1732 IAW A320 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM HARD POINT BETWEEN FR65 TO FR67, Y920. REPLACED FLOORBEAM HARD POINT BETWEEN FR65 TO FR67, Y920 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, Y765 IAW A320 SRM 51-72-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON SUPPORT FRAME WEB BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME WEB BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 16 INCHES, Y1295. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 16 INCHES, Y1295 IAW A320 SRM 51-72-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON SUPPORT FRAME WEB BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME WEB BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR62 TO FR63, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR62 TO FR63, S38L IAW A320 SRM 51-72-11.

Part: COVER — CRACKED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CRACK ON COVER SHEET TRAY BETWEEN FR68 TO FR69, Y1762. REPLACED COVER SHEET TRAY BETWEEN FR68 TO FR69, Y1762 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON L-2 DOOR SILL BETWEEN FR66 TO FR67, Y1732. REPAIRED L-2 DOOR SILL BETWEEN FR66 TO FR67, Y1732 IAW A320 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 6,566 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, -Y1465. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, -Y1465 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 +16 INCHES, -Y1245. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 +16 INCHES, -Y1245 IAW A320 SRM 51-72-11.

Part: COVER — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON COVER SHEET TRAY BETWEEN FR68 TO FR69, Y1732. REPLACED COVER SHEET TRAY BETWEEN FR68 TO FR69, Y1732 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 16 INCHES TO FR69 + 4 INCHES, -Y1165. REPLACED FLOORBEAM BETWEEN FR67 + 16 INCHES TO FR69 + 4 INCHES, -Y1165 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, Y1162 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT BEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y1292. REPLACED SEAT BEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y1292 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR52 TO FR53, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR52 TO FR53, S38L IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE ASSEMBLY BETWEEN FR48 TO FR49, S38R. REPLACED SHEAR PLATE ASSEMBLY BETWEEN FR48 TO FR49, S38R IAW A320 SRM 51-72-11.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 41,706 hrs · 17,224 cycles

FLT 306 CLT-LAS - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW PRESSURE (1400PSI) 9C OUTSIDE TEMP. MAINTENANCE CHARGED EMERGENCY OPERATION CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 41,706 hrs · 17,224 cycles

FLT 306 CLT-LAS - EMERGENCY EQUIPMENT - R2 DOOR ASSIST BOTTLE LOW PRESSURE (1500 PSI) 9C OUTSIDE TEMP. MAINTENANCE CHARGED EMERGENCY OPERATION CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 41,768 hrs · 17,244 cycles

SAL - C2 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR50 TO FR51, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR50 TO FR51, S38L IAW A320 SRM 51-72-11.

Part: BEARING — DAMAGED (NLG STEERING) · airframe 41,438 hrs · 17,129 cycles

FLT 339 PHX-MZT - UNSCHEDULED LANDING - CREW RECEIVED ACARS MESSAGE FOR BSCU/NOSE WHEEL STEERING PROBLEM. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX. MAINTENANCE REPLACED THE NOSE LANDING GEAR LEG. VENDOR REPLACED AN OVER-SIZED BEARING PER COMPONENT MM 32-27-02.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,501 hrs · 16,789 cycles

FLT NR 251 PHL-PHX EMERGENCY EQUIPMENT. EMERGENCY FLASHLIGHT INOPERATIVE AT AFT RT FLIGHT ATTENDANT SEAT. MX R&R THE FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 39,123 hrs · 76,321 cycles

SAL - MAJOR REPAIR - C1 CHECK - WATER TRAPPED IN THE RIGHT ELEVATOR UPPER SURFACE SKIN AT RIB 1 AND RIB 5. REPAIRED THE RIGHT ELEVATOR UPPER SURFACE SKIN AT RIB 1 AND RIB 5 IAW A320 SRM 55-21-11 AND 51-77-13.

Part: HINGE FITTING — WORN (RUDDER) · airframe 39,123 hrs · 16,321 cycles

SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE FITTING NR 2 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STATION 1926 / RIB 4 IAW A320 AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 39,123 hrs · 16,321 cycles

SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE FITTING NR 5 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2985 / RIB 7. REPLACED RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985 / RIB 7 IAW A320 AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 39,123 hrs · 76,321 cycles

SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE NR 4 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED RUDDER HINGE NR 4, VERTICAL STABILIZER STATION 2632 / RIB 6 IAW A320 AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 39,123 hrs · 76,321 cycles

SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE NR 3 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2279 / RIB 5. REPLACED RUDDER HINGE NR 3, VERTICAL STABILIZER STATION 2279 / RIB 5 IAW A320 AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 39,123 hrs · 76,321 cycles

SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE NR 1 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 780 / RIB 2. REPLACED RUDDER HINGE NR 1, VERTICAL STABILIZER STATION 780 / RIB 2 IAW A320 AMM 55-36-41.

Part: HINGE PIN — CORRODED (ZONE 500) · airframe 34,164 hrs · 14,370 cycles

SAL - CORROSION ON LEFT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9. REPLACED LEFT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9 IAW AWA TASKCARD C3L57322.

Part: CHANNEL — CRACKED (ZONE 500) · airframe 34,164 hrs · 14,370 cycles

SAL - CRACK ON LEFT WING AILERON LOWER SURFACE TRAILING EDGE PLATE, 16" FROM OUTBOARD END, WS 1166, RIB 22. REPLACED LEFT WING AILERON LOWER SURFACE TRAILING EDGE PLATE, 16" FROM OUTBOARD END, WS 1166, RIB 22 IAW A320 SRM 51-72-11.

Part: HINGE PIN — CORRODED (NR 2 SPOILER) · airframe 34,164 hrs · 14,370 cycles

SAL - CORROSION ON LEFT WING NR 2 SPOILER INBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9. REPLACED LEFT WING NR 2 SPOILER INBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9 IAW AWA TASKCARD C3L57322.

Part: HINGE PIN — CORRODED (SPOILER) · airframe 34,164 hrs · 14,370 cycles

SAL - CORROSION ON RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 6699, RIB 12. REPLACED RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 6699, RIB 12 IAW A320 AMM 27-64-43.

Part: HINGE PIN — CORRODED (ZONE 600) · airframe 34,164 hrs · 14,370 cycles

SAL - CORROSION ON RIGHT WING NR 5 SPOILER INBOARD HINGE PIN, WS 10729. REPLACED RIGHT WING NR 5 SPOILER INBOARD HINGE PIN, WS 10729 IAW A320 AMM 27-64-42.

Part: HINGE PIN — CORRODED (SPOILER) · airframe 34,164 hrs · 14,370 cycles

SAL - MAJOR REPAIR - CORROSION ON RIGHT WING NR 3 SPOILER OUTBOARD HINGE PIN, WS 7792, RIB 14. REPLACED RIGHT WING NR 3 SPOILER OUTBOARD HINGE PIN, WS 7792, RIB 14 IAW A320 AMM 27-64-43.

Part: HINGE PIN — CORRODED (ZONE 600) · airframe 34,164 hrs · 14,370 cycles

SAL - CORROSION ON RIGHT WING NR 4 SPOILER OUTBOARD HINGE PIN,WS 9235 - WS 9704. REPLACED RIGHT WING NR 4 SPOILER OUTBOARD HINGE PIN, WS 9235 - WS 9704 IAW A320 AMM 27-64-42.

Part: HINGE PIN — CORRODED (ZONE 600) · airframe 34,164 hrs · 14,370 cycles

SAL - CORROSION ON RIGHT WING NR 2 SPOILER INBOARD HINGE PIN, WS 6132 - WS 6699. REPLACED RIGHT WING NR 2 SPOILER INBOARD HINGE PIN, WS 6132 - WS 6699 IAW A320 AMM 27-64-42.

Part: FITTING — CORRODED (ZONE 200) · airframe 34,164 hrs · 14,370 cycles

SAL - MAJOR REPAIR - CORROSION ON THE R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16+6", S23R. REPLACED THE R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16+6", S23R IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 34,164 hrs · 14,370 cycles

SAL - MAJOR REPAIR - CORROSION ON L2 DOOR CUT OUT CENTER FITTING (SHAPE SILL), FR 68 -14", S23L. REPLACED L2 DOOR CUT OUT CENTER FITTING (SHAPE SILL), FS 68 -14", S23L IAW A320 SRM 51-72-11.

Part: SWITCH — FAILED (HYDRAULIC SYS) · airframe 33,242 hrs · 14,007 cycles

ORD - PHX - IN CRUISE FLIGHT, ECAM Y RSVR LO LVL MESSAGE, PERFORMED ECAM PTU OFF AND ENG PUMP OFF, SYSTEM RESET. THE CREW DECLARED A PRECAUTIONARY EMERGENCY. AS A PRECAUTIONARY MEASURE MAINTENANCE REPLACED THE LOW LEVEL SWITCH ASSEMBLY FOR THE YELLOW HYDRAULIC SYSTEM RESERVOIR IAW MM 29-13-41-400-004.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 32,784 hrs · 13,821 cycles

BOS - EE - LOG - 7401419 - WHILE ON BOARD THE AIRCRAFT, THE CLEANING CREW DEPLOYED THE R1 DOOR SLIDE. MAINTENANCE REPLACED THE R1 DOOR SLIDE IAW R1C25305.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED CORROSION ON CORNER FITTING LOWER SILL, FRAME 20 AT BL Y1975L. NO ALLOWABLE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING AT FRAME 20 AND Y1975L IAW AIRBUS 320 SRM 51-72-11 PAGE 1.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON AT LOWER SILL LOCATED FROM FS 65 TO FS 68 AT Y1250. RE-WORK WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14. MAINTENANCE CUT OUT DAMAGED SECTION ON LOWER SILL IAW AIRBUS 320 SRM 53-41-14. FABRICATED ANGLES AND FILLERS IAW AIRBUS 320 SRM 53-41-14 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE LOWER SILL FROM FS 65 TO FS 68 AND Y1250 IAW AIRBUS 320 SRM 53-41-14.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED LEVEL 2 CORROSION ON SHEAR PLATE LOCATED AT Y1305, FROM FS 69 TO FS 70. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW SHEAR PLATE LOCATED AT Y1305 FROM FS 69 TO FS 70 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y1165, BETWEEN FS 67+16" AND FS 69+4". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 67+16" TO FS 69+4" AND AT Y1165 IAW AIRBUS 320 SRM 51-72-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED CORROSION ON PLATE SUPPORT FLOOR STRUCTURE LOCATED AT Y-1732, FROM FS 69 TO FS 70. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW PLATE SUPPORT ON FLOOR STRUCTURE LOCATED AT Y-1732 FROM FS 69 TO FS 70 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y510 AND AT FS 66+5". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 64 TO FS 70 AND AT Y510 IAW AIRBUS 320 SRM 51-72-11.

Part: PLATE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED 4 INCH CRACK ON PLATE/TRAY LOCATED AT Y1306 AND BETWEEN FR 68 AND FR 68+12". NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW PLATE/TRAY AT Y1306 AND BETWEEN FS 68 AND FS 68+12 IAW AIRBUS 320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL- MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON RIVET AND CORNER SILL PLATE. CORNER SILL FRAME 20R REPLACED IAW A320 SRM 51-72-11 PAGE 1-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y765 AND AT FS 68. MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 68 AND AT Y765 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON AT LOWER SILL LOCATED FROM FS 67+19" AT Y-1292. RE-WORK WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14. MAINTENANCE CUT OUT DAMAGED SECTION ON LOWER SILL IAW AIRBUS 320 SRM 53-41-14. FABRICATED ANGLES AND FILLERS IAW AIRBUS 320 SRM 53-41-14 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE LOWER SILL FROM FR67+16" TO FR67+19" AND Y-1292 IAW AIRBUS 320 SRM 53-41-14.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON ANGLE FLOOR PROFILE ASSY AT Y465 AND FS 66. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW ANGLE AT Y465 BETWEEN FS 64 AND FS 66 IAW AIRBUS SRM 320 51-21-11 AND DWG D53472094.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON DUMMY RAIL, UPPER SURFACE BETWEEN FS 15 AND FS 20 LOCATED AT Y-254. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FS 12 TO FS 24 AT Y-254 IAW AIRBUS 320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y1165 AND AT FR 67+16". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 68 AND AT Y1165 IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

CORROSION ON SEAT TRACK Y 765 BETWEEN FRAME 15 AND FRAME 17. REPLACED IAW SRM A320 51-72-11 PAGE1-2. FASTENERS REMOVED AND INSTALLED IAW SRM A320 51-42-11 PARA. 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-765 AND AT FS 67+16". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 70 AND AT Y-765 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOOR SUPPORT, UPPER SURFACE, BETWEEN FS 15 AND FS 21, LOCATED AT Y254. RE-WORK ON FLOOR SUPPORT WAS OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SUPPORT BETWEEN FS 12 AND FS 24 AT Y254 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y 1582 AND BETWEEN FS 65 TO FS 66. MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 65 TO FS 66 AND AT Y1582 IAW AIRBUS 320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED LEVEL 2 CORROSION ON LOWER SILL BRACKET FROM FORWARD PASSENGER LT DOOR. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING ON THE FORWARD LT PASSENGER DOOR IAW AIRBUS 320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-1292 AND AT FS 65+21". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 64 TO FS 66 AND AT Y-1292 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y765 AND AT FS 64+10". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 66 AND AT Y765 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y919, FROM FS 66 TO FS 66+6". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 65 TO FS 67 AND AT Y919 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-1292 AND AT FS 67+7". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 66 TO FS 68 AND AT Y-1292 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y1165 AND FS 66. MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 64 TO FS 66 AND AT Y1292 IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON SUPPORT FLOOR TRACK AT Y-189 AND FROM FR 20 TO FR 24. MAINTENANCE REMOVED CORROSION AND FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS SRM 320 53-11-14. REMOVED AND INSTALLED NEW SUPPORT FLOOR TRACK AT Y-189 AND FROM FR 20 TO FR 24 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOORBEAM LOCATED AT Y-1292 AND AT FS 68+8". MAINTENANCE FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-1A FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM FROM FS 68 TO FS 69 AND AT Y-1292 IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED LEVEL 2 CORROSION ON DUMMY RAIL, UPPER SURFACE BETWEEN FS 12 AND FS 16 LOCATED AT Y503.2. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FR 12 TO FR 16 AT Y503.2 IAW AIRBUS 320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,961 hrs · 13,025 cycles

SAL - MAJOR REPAIR - DURING C7 CHECK DISCOVERED CORROSION ON DUMMY RAIL AT FS 16 AND Y-81. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FS 12 TO FS 16 AT Y-81 IAW AIRBUS 320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

MCN - AT "C" CHECK DISCOVERED CORROSION ON SEAT TRACK Y-765 BETWEEN FRAME 20 AND FRAME 21. NO ALLOWABLE DAMAGE LIMITS WERE FOUND. SEAT TRACK WAS REMOVED AND REPLACED FROM FROM FRAME 12 TO FRAME 24 IAW AIRBUS SRM A320 51-42 -11, PAGE 1-22. CPCP PROTECTION WAS APPLIED PER AIRBUS SRM 51-21-00.

Part: CONTROL UNIT — MALFUNCTIONED (SERVO CONTROL)

DEPARTING PHX, EN ROUTE TO SAN, CREW REPORTED DURING LEVEL OFF GOING THROUGH 330 KTS IAS AT 220K FT MSL AIRPLANE SHOOK ON LONG AXIS AT ABOUT 4-10 CYCLES PER SECOND SHAKING STOPPED BELOW 300KTS IAS. AIRCRAFT DECLARED EMERGENCY AND LANDED IN SAN WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT IAW AIRBUS 320 TROUBLE SHOOTING MANUAL 27-34-00-200 AND 05-50-00-810-801. REMOVED AND REPLACED THE RT INBOARD, YELLOW, ELEVATOR SERVO CONTROL PER AIRBUS 320 MM 27-34-51-000-001 AND 27-34-51-400-001. VENDOR CONFIRMED FAILURE. FOUND EXCESSIVE OSCILLATING, AND BOTH SPHERICAL BEARINGS FLATTENED OUT. ALSO FOUND INSULATION RESISTANCE TO LOW. UNIT WAS REPAIRED AND TESTED IAW CMM 27-34-52 REV.9.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,712 hrs · 12,257 cycles

FOUND EMERGENCY LIGHTS AT PASSENGER SEATS 9L AND 11L ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT MID CABIN EMERGENCY LIGHT BATTERY IAW AMERICA WEST AIRLINES T/C A1C33302. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,576 hrs · 12,204 cycles

DURING 4 DAY CHECK BOTH EMERGENCY EXIT LIGHTS IN THE FORWARD GALLEY WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD POWER SUPPLY IAW TC R1433303 AND TC A1C33302. OPERATIONAL CHECK NORMAL.

Part: PROXIMITY SENSOR — FAULTY (ZONE 711) · airframe 27,389 hrs · 11,742 cycles

PHX - LANDING GEAR - AFTER DEPARTING PHX EN ROUTE TO LAS ECAM INDICATED THE LANDING GEAR WAS NOT UP AND LOCKED, FLIGHT CREW CONFIRMED THAT NLG GEAR WAS DOWN BY NOISE LEVEL AND INDICATIONS, RECYCLED THE LANDING GEAR PER ECAM INSTRUCTIONS AND GEAR RETRACTED, PROCEEDED TO LAS AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX AND MAINTENANCE FOUND NLG PROXIMITY SENSORS 24GA & 25GA Z DIMENSIONS EXCEED LIMITS. REMOVED AND REPLACED PROXIMITY SENSOR 24GA IAW AMM 32-31-33, AND ADJUSTED BOTH SENSORS. PERFORMED LANDING GEAR RETRACTION CHECK, NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2

SAL - MAJOR REPAIR - DURING C-07 CHECK, CORROSION ON SEAT TRACK WAS FOUND AT Y 1292, BETWEEN FRAMES 15-AND 20 IN THREE PLACES. SEAT TRACK WAS REPLACED IAW AIRBUS SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,691 hrs · 13,025 cycles

SAL - DURING C-07 CHECK, CORROSION FOUND ON SEAT TRACK Y-1292 BETWEEN FRAME 15 AND FRAME 22 IN 5 PLACES. SEAT TRACK WAS REPLACED IAW A320 51-72-11 PAGE 1-2.

Part: BATTERY — DISCHARGED (ZONE 221) · airframe 26,836 hrs · 11,514 cycles

PHX - EEL - DURING 4-DAY CHECK THE LT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED BATTERY AT LEFT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.

Part: WINDSHIELD — CRACKED (FUSLEAGE) · airframe 26,540 hrs · 11,394 cycles

EN ROUTE, AT FL 370 THE FO`S WINDSHIELD CRACKED WHEN HEATING ELEMENT BURNED THROUGH, DIVERTED INTO ABQ & LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM, & WINDOW HEAT COMPUTER, OPERATIONAL TEST GOOD. FAILURE ANALYSIS OF WINDSHIELD, OUTBOARD GLASS PLY FRACTURED WITH ORIGIN OF FRACTURE 4.9 INCHES FROM AFT EDGE & 9.8 INCHES FROM BOTTOM EDGE OF WINDSHIELD. AN ELECTRICAL ARC PATH ORIGINATED AT BOTTOM CONDUCTIVE BUSS BAR & TRAVELED ACROSS HEATING FILM VISION AREA OF WINDSHIELD TO ORIGIN OF FRACTURE. IN AREA SURROUNDING BOTTOM CONDUCTIVE BUSS BAR EVIDENCE OF MOISTURE INGRESSION NOTED. MOISTURE INGRESSION ALSO NOTED IN SEVERAL OTHER LOCATIONS AROUND WINDOW.

Part: PROXIMITY SENSOR — FAULTY (FWD CARGO DOOR) · airframe 25,722 hrs · 11,072 cycles

AIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ECAM WARNING FOR FORWARD CARGO DOOR WARNING INDICATION, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED FORWARD CARGO DOOR AND FOUND IT SECURE, ISSUED MEL 52-70-01, COND. 1 (FWD CARGO DOOR INDICATION INOP), ORDERED PROXIMITY SENSOR. MAINTENANCE FOUND FORWARD CARGO DOOR PROXIMITY SENSOR POSITION TARGET OUT OF ADJUSTMENT; ADJUSTED TARGET IAW AMM 52-71-00-05, OPERATIONAL CHECK WAS GOOD.